Global Patent Index - EP 1088754 A2

EP 1088754 A2 20010404 - Composite helicopter rotor yoke

Title (en)

Composite helicopter rotor yoke

Title (de)

Hubschrauberrotorarm aus Faserverbundstoff

Title (fr)

Etrier pour rotor d'hélicoptère en matériaux composites

Publication

EP 1088754 A2 20010404 (EN)

Application

EP 00203352 A 20000927

Priority

US 40769199 A 19990928

Abstract (en)

The protective edge member (51, 53) for use on a composite flexure, such as a helicopter main rotor yoke (11), having an exposed edge surface (24), comprises an innermost composite ply (57) attached to the exposed edge surface (24), an outermost composite ply (59) attached to the innermost composite ply (57); and at least one interior composite ply (55) disposed between the innermost composite ply (57) and the outermost composite ply (59). <IMAGE> <IMAGE>

IPC 1-7

B64C 27/33

IPC 8 full level

B64C 27/35 (2006.01); B64C 27/33 (2006.01); B64C 27/46 (2006.01)

CPC (source: EP KR US)

B64C 27/33 (2013.01 - EP US); B64C 27/46 (2013.01 - KR); Y10T 29/49318 (2015.01 - EP US); Y10T 29/49337 (2015.01 - EP US); Y10T 428/24785 (2015.01 - EP US)

Designated contracting state (EPC)

DE FR GB IT

DOCDB simple family (publication)

EP 1088754 A2 20010404; EP 1088754 A3 20020403; EP 1088754 B1 20030326; CA 2320606 A1 20010328; CA 2320606 C 20090224; DE 1088754 T1 20011011; DE 60001784 D1 20030430; DE 60001784 T2 20031204; JP 2001122195 A 20010508; KR 100726201 B1 20070611; KR 20010050665 A 20010615; US 6375426 B1 20020423

DOCDB simple family (application)

EP 00203352 A 20000927; CA 2320606 A 20000926; DE 00203352 T 20000927; DE 60001784 T 20000927; JP 2000293303 A 20000927; KR 20000056687 A 20000927; US 40769199 A 19990928